DELTA 1 R/B, 2661

Orbit data source: Space-Track

DELTA 1 R/B, 2661 is space debris in SSO originally from a launch on Thu, 26 Jan 1967 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
2661, 1967-006B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1967-01-26 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 DELTA 1 R/B
1  2661U 67006B   26106.45996538 -.00000030  00000-0  91164-4 0  9997
2  2661 101.9246 183.9740 0065199 176.2815 195.3361 12.68024049740333
Epoch: 2026-04-16T11:02Z
TLE epoch observation values (Epoch: 2026-04-16T11:02:21.008Z)
Latitude
11.12964°
Longitude
171.40991°
Altitude
1,440.715 km
Speed
7.12 km/s
True Right ascension
12h 06m 25s
True Declination
11° 04' 13"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:51:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,438.164 km
Perigee altitude
1,336.902 km
Semi-major axis
7,765.67 km
Eccentricity
0.00652
Inclination
101.9246°
RAAN
183.974°
Arg. of periapsis
176.2815°
True anomaly
195.14004°
Mean anomaly
195.3361°
Eccentric anomaly
195.23792°
Mean motion
3.17157 °/min
Orbital period
113.51 mins
BSTAR
0.000091164
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Other satellites on launch #6 in the year 1967 (1967-01-26 UTC)

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